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MSFS 2024 · General Aviation
Pilatus PC-12 Startup Checklist
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FLIGHT2.17.0Checklist
Pilatus PC-12MSFS 2024 · Startup Checklist · 256 steps · 22 phases
PHS 1 - Pre-Flight Planning8 steps
| 01 | Aircraft VariantPC-12 NGX (PT6E-67XP) CONFIRMEDCAUTION: This checklist follows the PC-12/47E POH for MSN 2001 and up (PC-12 NGX, PT6E-67XP with EPECS). The earlier PC-12 NG (PT6A-67P) uses a separate condition lever and a manual start sequence and does not match these steps. | |
| 02 | Weather Briefing (METAR / TAF)REVIEWEDNOTE: The PC-12/47E is approved for flight into known icing. Review icing, ceiling, visibility and alternates. | |
| 03 | NOTAMsREVIEWED | |
| 04 | Fuel RequiredCALCULATEDNOTE: Total fuel capacity 406.8 US gal, 2736.5 lb (1540 litres, 1241.3 kg). Total usable 402 US gal, 2703.6 lb (1521.5 litres, 1226.4 kg). | |
| 05 | Weight and BalanceWITHIN LIMITSCAUTION: MRW 10,495 lb (4760 kg), MTOW 10,450 lb (4740 kg), MLW 9,921 lb (4500 kg), MZFW 9,039 lb (4100 kg). | |
| 06 | Takeoff PerformanceCALCULATEDNOTE: Maximum demonstrated crosswind (not a limitation): 30 kts flaps 0, 25 kts flaps 15, 20 kts flaps 30, 15 kts flaps 40. | |
| 07 | Route / Flight PlanPREPARED AND LOADEDNOTE: Honeywell Primus Apex avionics. Engine inlet altitude range sea level to 30,000 ft. | |
| 08 | ATISOBTAINED |
PHS 2 - Preflight Inspection - Empennage22 steps
| 01 | LuggageCHECKED AND SECURED | |
| 02 | Cargo (Combi Interior)CHECK AGAINST RETAINER ANGLESNOTE: Cargo located against retainer angles installed on the seat rails. | |
| 03 | Tie Down Straps (Combi Interior)CHECK FITTINGS AND TENSION | |
| 04 | Cargo DoorCLOSED AND LOCKED - CHECK GREEN FLAGSNOTE: After cargo loading or unloading also check the lower attachment lugs for condition. | |
| 05 | Static Ports and SkinCHECKEDCAUTION: RVSM critical area: inspect the static port plates and 18 in forward, 6 in aft, 8 in above and 6 in below. No paint ridges, corrosion, elongation, deformation or foreign matter. | |
| 06 | Tail Tie-DownDISCONNECTED | |
| 07 | External Power DoorCLOSED / AS REQUIRED | |
| 08 | Oxygen Rupture DiscINTACTNOTE: If a larger capacity oxygen system is installed in the rear fuselage. | |
| 09 | Rudder and Trim TabCHECK VISUALLY | |
| 10 | Vertical StabilizerCHECK VISUALLY | |
| 11 | Elevator AssemblyCHECK VISUALLY | |
| 12 | Horizontal StabilizerCHECK VISUALLY - TRIM MARK IN GREEN RANGE | |
| 13 | Deicing BootsCHECK VISUALLY | |
| 14 | Static Discharge WicksCHECK | |
| 15 | Dorsal and Ventral FairingsCHECK | |
| 16 | Battery Compartment - LDR Circuit BreakerCHECK IN | |
| 17 | Battery Compartment - ELTCHECK CONDITION | |
| 18 | Battery Compartment - Autopilot Servos and CablesCHECK CONDITION | |
| 19 | Battery Compartment - Power Junction Box Circuit BreakersCHECK IN | |
| 20 | Steering BarSTOWED AND SECURED | |
| 21 | BatteryCONNECTED | |
| 22 | Battery CompartmentCHECK CLOSED |
PHS 3 - Preflight Inspection - Right Wing13 steps
| 01 | FlapsCHECK CONDITION | |
| 02 | Aileron and Flettner TabCHECK CONDITION | |
| 03 | Fuel Tank Vents (three)CLEAR OF OBSTRUCTIONS | |
| 04 | Static Discharge WicksCHECK SECURITY AND CONDITION | |
| 05 | Nav / Strobe LightCHECK CONDITION | |
| 06 | Fuel Quantity and Filler CapCHECK AND SECURE | |
| 07 | Pitot ProbeCOVER REMOVED AND CHECKED | |
| 08 | AOA ProbeCOVER REMOVED AND CHECK FREE MOVEMENT | |
| 09 | Wing Tie-Down / Wheel ChocksDISCONNECTED AND REMOVED | |
| 10 | De-Icing BootCHECK GENERAL CONDITION | |
| 11 | Right Main Landing GearCHECK | |
| 12 | Right Brake AssemblyCHECK | |
| 13 | Two Fuel DrainsSAMPLE AND SECURE |
PHS 4 - Preflight Inspection - Nose Section19 steps
| 01 | Service Bay (right) - Oxygen PressureCHECKNOTE: If a standard oxygen system is installed. | |
| 02 | Service Bay (right) - Oxygen and ECS DoorsCLOSED | |
| 03 | Service Bay (right) - Oxygen Rupture DiscINTACT | |
| 04 | Cowling RHCHECK AND SECURE | |
| 05 | Propeller Blade AnchorREMOVED AND STOWED | |
| 06 | Propeller BladesCHECKNOTE: The manual recommends keeping a copy of Hartzell Service Letter 61-360 (latest issue) in the aircraft for damage assessment. | |
| 07 | Propeller De-Icing BootsCHECK GENERAL CONDITION | |
| 08 | Propeller SpinnerCHECK | |
| 09 | Air Inlet and Exhaust CoversREMOVED AND STOWED | |
| 10 | Air InletsCHECK ENGINE AIR INTAKE, OIL COOLER, ECS AND GENERATOR CLEAR | |
| 11 | Exhaust SystemCHECK | |
| 12 | Nose Gear and DoorsCHECK | |
| 13 | Wheel ChocksREMOVED | |
| 14 | Engine Drain Mast (LH)CHECK - NO LEAKS PERMITTED | |
| 15 | Engine Drain (LH)SAMPLE AND SECURE | |
| 16 | Oil QuantityCHECK SIGHT GLASS AND DIPSTICKWARNING: Do not touch output connectors or coupling nuts of the ignition exciter with bare hands.NOTE: Check oil level in the green range of the sight glass within 10 to 20 minutes after shutdown. Total oil capacity 3.6 US gal (13.6 litres); operating range 1.0 US gal (3.8 litres). Takeoff is not approved with ENGINE OIL LEVEL illuminated. | |
| 17 | Cowling LHCHECK AND SECURE | |
| 18 | WindshieldCHECK CLEAN | |
| 19 | Service Bay (left) DoorsCLOSED |
PHS 5 - Preflight Inspection - Left Wing13 steps
| 01 | Two Fuel DrainsSAMPLE AND SECURE | |
| 02 | Left Main Landing GearCHECK | |
| 03 | Left Brake AssemblyCHECK | |
| 04 | De-Icing BootCHECK GENERAL CONDITION | |
| 05 | Pitot ProbeCOVER REMOVED AND CHECKED | |
| 06 | AOA ProbeCOVER REMOVED AND CHECK FREE MOVEMENT | |
| 07 | Wing Tie-Down / Wheel ChocksDISCONNECTED AND REMOVED | |
| 08 | Fuel Quantity and Filler CapCHECK AND SECURE | |
| 09 | Nav / Strobe LightCHECK CONDITION | |
| 10 | Static Discharge WicksCHECK SECURITY AND CONDITION | |
| 11 | Fuel Tank Vents (three)CLEAR OF OBSTRUCTIONS | |
| 12 | Aileron and Trim TabCHECK CONDITION | |
| 13 | FlapsCHECK CONDITION |
PHS 6 - Preflight Inspection - Cabin8 steps
| 01 | Passenger DoorCLOSED AND LOCKED - CHECK 6 GREEN FLAGS | |
| 02 | Hand LuggageSECURED / STOWED | |
| 03 | Passenger SeatsBACKRESTS UPRIGHT | |
| 04 | Passenger Seat BeltsFASTENED | |
| 05 | Overwing Emergency ExitLOCK PIN REMOVED, EXIT CHECKED AND LOCKED | |
| 06 | Fire ExtinguisherCHECK ATTACHMENT AND PRESSURE | |
| 07 | Passenger Oxygen MasksCONNECTED AND STOWEDNOTE: Required for each passenger for flights above 10,000 ft. | |
| 08 | Flight Control LockREMOVED AND PLACED IN STOWAGE POINT |
PHS 7 - Before Starting Engine27 steps
| 01 | Preflight InspectionCOMPLETE | |
| 02 | STBY BUS SwitchONNOTE: Wait until the MFD powers up (about 30 seconds) before switching the batteries on. | |
| 03 | Display Reversion Control PanelPILOTS PFD NORM / CO-PILOTS PFD NORM | |
| 04 | ATIS and Start Up ClearanceRECEIVED | |
| 05 | FMS ProgrammingCOMPLETED | |
| 06 | SeatsADJUSTED AND LOCKED | |
| 07 | Seat BeltsFASTENED | |
| 08 | EPS SwitchTEST - MINIMUM 5 SECONDS | |
| 09 | EPS Green TEST IndicatorON DURING TEST | |
| 10 | EPS SwitchARMED | |
| 11 | EPS Red EPS ON IndicatorON | |
| 12 | EPS ESISALIGNING | |
| 13 | BAT 1 and BAT 2 SwitchesON | |
| 14 | Red EPS ON IndicatorCHECK OFF | |
| 15 | BAT 1 and BAT 2 IndicatorsCHECK 24 VDC MINIMUM | |
| 16 | External Power Unit (if available)ON - CHECK 28 VDC | |
| 17 | External Power UnitCONNECT - CHECK OHP AVAIL ON | |
| 18 | EXT PWR SwitchON | |
| 19 | BAT 1 and BAT 2 IndicatorsCHECK 28 VDCNOTE: The aircraft external power control unit disconnects the EPU if output voltage is above 29.5 or below 22 VDC. | |
| 20 | Landing Gear 3 GreensCHECK | |
| 21 | FUEL QuantitySUFFICIENT FOR FLIGHT - BALANCED WITHIN 3 SEGMENTS | |
| 22 | FIRE WARN Test SwitchPUSH | |
| 23 | LAMP Test SwitchPUSH | |
| 24 | Oxygen Pressure GageCHECK 1,850 PSI MAX | |
| 25 | PASSENGER OXYGEN SelectorAUTONOTE: Set the switch to OFF if no passengers are on board. | |
| 26 | Direct Vision WindowCLOSED AND LOCKED | |
| 27 | Radios / AvionicsSET AS REQUIRED - ESIS ALIGNED |
PHS 8 - Engine Start17 steps
| 01 | External LightsAS REQUIREDNOTE: Avoid prolonged use of the beacon and logo lights, which decreases battery power and can affect engine starting. | |
| 02 | Propeller AreaCLEAR - CONFIRM CLEAR OF OBSTRUCTIONS | |
| 03 | CAS WindowCHECK NO DOOR, OIL TEMPERATURE OR CYAN AUTOPILOT MESSAGESCAUTION: Do not make control inputs or start the engine before the cyan autopilot messages extinguish, or autopilot availability in the air may be affected. | |
| 04 | Engine SwitchRUNNOTE: The EPECS automatically aborts a start on ITT exceedance, hung start, no light-off, or if the starter switch is pushed during the sequence, and commands a 30 second dry motor run. | |
| 05 | Fuel WindowCHECK TWO GREEN PUMP INDICATIONS | |
| 06 | STARTER SwitchPUSH MOMENTARILY | |
| 07 | Oil PressureCHECK RISING | |
| 08 | Ng approx 16%CHECK LIGHT UP | |
| 09 | ITTMONITORWARNING: Start ITT maximum 1000 degC. 900 to 1000 degC for a maximum of 5 seconds; 850 to 900 degC for a maximum of 20 seconds. | |
| 10 | STARTER Switch (rapid ITT rise toward 1000 degC, start not auto-aborted)PUSH MOMENTARILY | |
| 11 | NgSTABLE AT 64.5%NOTE: Minimum idle limits: ITT 750 degC, Ng 64.5%. | |
| 12 | STARTER Switch (if Ng stays below 50% and start not auto-aborted)PUSH MOMENTARILY | |
| 13 | Starter SequenceCOMPLETED | |
| 14 | Engine InstrumentsSTABLE IN GREEN RANGE | |
| 15 | GEN 1 and GEN 2CHECK VOLTS AND AMPS | |
| 16 | FUEL RESET Soft KeyPUSH TO RESET | |
| 17 | External Power Unit (if used)DISCONNECT |
PHS 9 - Before Taxiing20 steps
| 01 | Flaps Lever15 DEG | |
| 02 | ICE PROTECTION SwitchesALL ON FOR 1 MINUTENOTE: Required if icing conditions are expected or on the first flight of the day. Windshield to heavy. | |
| 03 | CAS WindowNO CAUTIONS - PROPELLER, INERT SEP AND BOOTS ON | |
| 04 | ICE PROTECTION SwitchesSET AS REQUIRED | |
| 05 | Inertial SeparatorOPEN IF ON UNPREPARED SURFACE OR FOR BIRD STRIKE PROTECTION | |
| 06 | PCL (stick pusher test)SET 5 - 10 PSI | |
| 07 | STICK PUSHER Test Switch (overhead)PUSH AND HOLD | |
| 08 | PCLSET TO IDLE | |
| 09 | Elevator ControlPULL | |
| 10 | Shaker / Break SequenceCHECK CORRECT OPERATIONNOTE: Shaker 2 sec, break 1 sec, shaker 2 sec, break 1 sec, then pusher and shaker. | |
| 11 | ICE PROTECTION PUSHER ICE MODE AdvisoryCHECK ON | |
| 12 | PUSHER INTR Switch (control wheel)PRESS AND HOLD - CHECK PUSHER INTERRUPTS | |
| 13 | STICK PUSHER Test SwitchRELEASE | |
| 14 | PusherCHECK OFF | |
| 15 | PusherCHECK ON AFTER 3 SECONDS - VISUAL AND AURAL | |
| 16 | PUSHER INTR SwitchRELEASE | |
| 17 | PusherCHECK OFF - VISUAL AND AURAL | |
| 18 | Elevator ControlCHECK FULL AND FREE MOVEMENT | |
| 19 | PFD, MFD, CAS, ESISNO FLAGS OR RED WARNINGS - ALL ALIGNED | |
| 20 | PFD Engine WindowCHECK T1NOTE: Engine takeoff power is calculated based on the displayed T1. |
PHS 10 - Taxiing6 steps
| 01 | EXTERNAL LIGHTS SwitchesAS REQUIRED | |
| 02 | PASSENGER WARNING Switches (if installed)ON | |
| 03 | Parking BrakeRELEASE | |
| 04 | BrakesCHECK | |
| 05 | PCLCHECK BETA AVAILABLE - RETURN TO IDLECAUTION: To avoid propeller damage, do not allow stabilized propeller operation between 350 and 900 RPM with the propeller not feathered. Do not leave the PCL stationary for more than 30 seconds in the beta range. | |
| 06 | Display UnitsCOMPARE ADI, SPEEDS, ALTITUDE, HEADING - NO FLAGS |
PHS 11 - Before Departure10 steps
| 01 | Takeoff Power SettingCALCULATEDNOTE: Takeoff rating 1200 SHP, torque 44.84 psi, ITT 850 degC, Ng 104%, Np 1700 RPM. Takeoff power is limited to 5 minutes. | |
| 02 | Engine InstrumentsCHECK | |
| 03 | Flaps15 DEGNOTE: Flaps 30 deg may be used for reduced takeoff distance. | |
| 04 | TrimSET GREEN RANGENOTE: Set to the green diamond if the CG is 236 inches (6 metres) or further aft of datum. | |
| 05 | Fuel QuantityCHECK | |
| 06 | CPCSCHECK FMS IDENTIFIER AND ELEV - NO CPCS FAULTS | |
| 07 | DC Amps BatteriesCHECK BAT 1 AND BAT 2 BELOW 30 AMPSCAUTION: If greater than 30 amps is indicated, delay takeoff until indications are at or below 30 amps. | |
| 08 | Flight ControlsFULL, FREE AND CORRECT | |
| 09 | Radios / Navigation / FD / ClearanceSET AND CHECKED | |
| 10 | Departure and Emergency BriefingCOMPLETED |
PHS 12 - Line Up Check7 steps
| 01 | PROBES SwitchON | |
| 02 | Windshield HeatAS REQUIRED | |
| 03 | INERT SEPAS REQUIRED | |
| 04 | External Light SwitchesAS REQUIRED | |
| 05 | TransponderAS REQUIRED | |
| 06 | RunwayIDENTIFIED - HEADING VERIFIED AND BUG SYNCHRONIZED | |
| 07 | CAS WindowCHECK |
PHS 13 - Takeoff9 steps
| 01 | ACS BLEED AIR SwitchINHIBITNOTE: Used if static takeoff torque is below flat rating and additional torque is required. | |
| 02 | POWER CONTROL LEVERSET TO T/OCAUTION: Monitor for exceedances. EPECS will not protect against all possibilities of exceedance.NOTE: The EPECS sets power to ambient conditions. | |
| 03 | Engine InstrumentsMONITOR TORQUE, ITT, GAS GENERATOR RPM, OIL TEMP AND PRESSUREWARNING: Takeoff limits: torque 44.84 psi, ITT 850 degC, Ng 104%, Np 1700 RPM, oil pressure 90 to 135 psi, oil temperature 15 to 110 degC. | |
| 04 | RotateVR THEN INITIAL CLIMB AT VX OR VYNOTE: VR is 82 KIAS with flaps 15 deg and 76 KIAS with flaps 30 deg at MTOW 10,450 lb (4740 kg), sea level ISA. | |
| 05 | Brakes (after lift-off, positive rate)PRESS TO STOP WHEEL ROTATION | |
| 06 | Landing Gear SelectorUPCAUTION: Maximum landing gear operating speed (VLO) 180 KIAS. | |
| 07 | Yaw DamperON | |
| 08 | Flaps0 DEG ABOVE 100 KIAS | |
| 09 | Taxi and Landing LightsOFF |
PHS 14 - Climb11 steps
| 01 | Ice Protection SystemAS REQUIRED | |
| 02 | AutopilotAS REQUIRED | |
| 03 | FMS Auto Speed (if selected)VERIFY AND CONFIRM CORRECT | |
| 04 | POWER CONTROL LEVERSET TO MCPCAUTION: Monitor for exceedances. EPECS will not protect against all possibilities of exceedance. | |
| 05 | ACS BLEED AIR SwitchAUTONOTE: If INHIBIT was selected for takeoff. | |
| 06 | Cabin PressureMONITOR | |
| 07 | TorqueMONITOR - MAX 44.8 PSI | |
| 08 | ITTMONITOR - MAX 825 DEGCWARNING: Maximum climb ITT limit is 825 degC. | |
| 09 | NgMONITOR - MAX 104% | |
| 10 | Baro (passing transition altitude)SET STD AND CROSS CHECK | |
| 11 | Climb Speed ReferenceVY 130 KIAS SL / 125 KIAS TO 15,000 FT / 120 KIAS ABOVE 20,000 FTCAUTION: If autothrottle is installed and engaged with FD/AP OFF, monitor for torque exceedances; levelling off below 18,000 ft in this state can command torque above the max cruise limit.NOTE: VX is 120 KIAS. Recommended climb speed with flaps retracted and Pusher Ice Mode is 135 KIAS. |
PHS 15 - Cruise9 steps
| 01 | Cabin PressurizationMONITOR | |
| 02 | POWER CONTROL LEVERSET AS REQUIREDNOTE: Cruise rating 1100 SHP, torque 40.63 psi, ITT 820 degC, Ng 104%, Np 1700 RPM. | |
| 03 | Engine InstrumentsMONITORCAUTION: VMO 240 KIAS at or below 16,300 ft; MMO 0.49 above, per the VMO schedule. | |
| 04 | Fuel StateMONITORNOTE: On longer flights the digital fuel quantity can be updated with the FUEL RESET soft key. Reset only wings level, pitch within 3 deg, unaccelerated and without turbulence. | |
| 05 | FMS Auto Speed (if selected)VERIFY AND CONFIRM CORRECT | |
| 06 | Ice Protection SystemAS REQUIRED | |
| 07 | RVSM - Cross Check AltimetersMAXIMUM DIFFERENCE 200 FEET | |
| 08 | RVSM - AltimetersRECORD INDICATED ALTITUDESNOTE: Record pilot, co-pilot and ESIS readings on entering RVSM airspace and hourly thereafter. | |
| 09 | RVSM - Autopilot / Altitude HoldVERIFY ALTITUDE HOLD WITHIN 65 FEET |
PHS 16 - Descent7 steps
| 01 | ATIS / BriefingRECEIVED / PERFORMED | |
| 02 | Ice Protection SystemAS REQUIRED | |
| 03 | POWER CONTROL LEVERSET TO DESIRED TORQUE | |
| 04 | FMS Auto Speed (if selected)VERIFY AND CONFIRM CORRECT | |
| 05 | CPCS System WindowCHECK LANDING FIELD ELEVATION SET | |
| 06 | PassengersBRIEF | |
| 07 | Passenger Warning Switches (if installed)ON |
PHS 17 - Approach Check9 steps
| 01 | AltimeterSET | |
| 02 | Ice Protection SystemAS REQUIRED | |
| 03 | Inertial SeparatorOPEN IF ON UNPREPARED SURFACE OR FOR BIRD STRIKE PROTECTION | |
| 04 | Fuel QuantityCHECK | |
| 05 | Landing GearDOWN BELOW 180 KIASCAUTION: VLO 180 KIAS; VLE 240 KIAS. | |
| 06 | Taxi and Landing LightsAS REQUIRED | |
| 07 | FlapsAS REQUIREDCAUTION: VFE 165 KIAS at or below 15 deg, 130 KIAS above 15 deg. With residual airframe ice set a maximum of 15 deg; with boot failure maintain 0 deg. | |
| 08 | SpeedAS INDICATED BY DYNAMIC SPEED BUG (1.3 VS) | |
| 09 | FMS Auto Speed (if selected)VERIFY AND CONFIRM CORRECT |
PHS 18 - Final Check5 steps
| 01 | Landing Gear3 GREEN LIGHTS | |
| 02 | Flaps40 DEG OR AS REQUIREDCAUTION: With residual airframe ice set a maximum of 15 deg; with boot failure maintain 0 deg. | |
| 03 | SpeedREDUCE TO DYNAMIC SPEED BUG (1.3 VS) AND STABILIZEDNOTE: Landing approach speeds at MLW 9,921 lb (4500 kg): flaps 0 deg 120 KIAS, flaps 15 deg 99 KIAS, flaps 30 deg 89 KIAS, flaps 40 deg 85 KIAS. Boot failure 130 KIAS; AOA deice or Pusher Ice Mode failure 105 KIAS. | |
| 04 | Cabin PressurizationDIFF PRESSURE BELOW 0.7 PSI DECREASING | |
| 05 | AP, AT (if installed), YDDISENGAGED PRIOR TO LANDINGNOTE: Use the red AP QD button on the yoke. |
PHS 19 - Landing7 steps
| 01 | AircraftTOUCH DOWN MAIN WHEELS FIRST | |
| 02 | AircraftDO NOT FLARE WITH HIGH PITCH ANGLE | |
| 03 | Power Control LeverIDLE DETENT | |
| 04 | BrakingAS REQUIRED | |
| 05 | Short Field - Power Control LeverREVERSECAUTION: Max reverse limits: 900 SHP, torque 34.26 psi, ITT 820 degC, Np 1650 RPM.NOTE: Short field procedure: touch down main wheels first, do not flare with high pitch angle, PCL to REVERSE, braking FIRM, then PCL to IDLE. | |
| 06 | Short Field - BrakingFIRM | |
| 07 | Short Field - Power Control LeverIDLE |
PHS 20 - After Landing6 steps
| 01 | FlapsUPNOTE: Actioned when the runway is vacated. | |
| 02 | TrimsSET GREEN RANGE | |
| 03 | External LightsAS REQUIRED | |
| 04 | Ice Protection SwitchesOFF OR AS REQUIRED | |
| 05 | TransponderSTBY OR CHECK GND | |
| 06 | WX RadarSTBY |
PHS 21 - Shutdown17 steps
| 01 | Power Control LeverIDLE DETENTWARNING: In case of engine fire, do the Engine Fire procedure (manual 3-7-02) instead.NOTE: Allow ITT to stabilize at least two minutes at ground idle. Monitor compressor deceleration after shutdown for possible engine damage. | |
| 02 | Parking BrakeSET / PEDALS PUSH | |
| 03 | ICE PROTECTION SwitchesOFF | |
| 04 | Inertial SeparatorOPEN IF ON UNPREPARED SURFACE | |
| 05 | Feather Inhibit Switch (if installed)PUSH AND HOLD IF DESIREDCAUTION: After 9 consecutive shutdowns using the propeller feather inhibit function, a normal engine shutdown must be performed. | |
| 06 | Engine SwitchOFFNOTE: If T1 is at or above approximately 23 degC the EPECS commands a momentary 15 second dry motoring cycle during shutdown. | |
| 07 | CAS Feather Inhibit StatusCHECK | |
| 08 | Feather Inhibit SwitchRELEASE | |
| 09 | External Lights SwitchesOFF | |
| 10 | PASS-Warning Switches (if installed)OFF | |
| 11 | Main OXYGEN LeverOFF | |
| 12 | Engine Oil LevelCHECK - REFILL WITH APPROVED OILNOTE: Minimum 60 seconds after shutdown. | |
| 13 | CPCSCHECK CABIN DEPRESSURIZED | |
| 14 | STBY BUS SwitchOFF | |
| 15 | EPS SwitchOFF | |
| 16 | Battery 1 and 2 SwitchesOFF | |
| 17 | Crew Oxygen MasksCHECK 100%NOTE: If the oxygen system was used. |
PHS 22 - Parking6 steps
| 01 | Flight Control LockINSTALLED | |
| 02 | Wheel ChocksAS REQUIRED | |
| 03 | Tail StandAS REQUIREDNOTE: Install the tail stand when the aircraft is parked outside and wet snowfall is expected. | |
| 04 | Tie DownsAS REQUIRED | |
| 05 | Propeller AnchorINSTALLEDCAUTION: Make sure the propeller anchor is properly installed to prevent engine damage from windmilling with zero oil pressure. | |
| 06 | External CoversINSTALLED |